Afterburning of High-Temperature Products of Incomplete Combustion in a Supersonic Flow upon a Secondary Injection of Oxidizer,

Abstract

The article is an examination of the results of an experimental study in the afterburning of a supersonic flow of products that have not completely burned on account of re-injected oxidizers HNO3 and N2O4.

Document Details

Document Type
Technical Report
Publication Date
Apr 17, 1974
Accession Number
AD0779623

Entities

People

  • A. M. Rusak
  • I. S. Saburov
  • L. F. Shaikhinurova
  • V. M. Klevanskii
  • Z. G. Shaikhutdinov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Afterburning
  • Chemical Reactions
  • Combustion
  • Exothermic Reactions
  • Flow
  • High Temperature
  • Secondary Injection
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow